19980925037739A

Accident · Substantial damage

FAA accident report · Cessna 210L · Orlando, FL · September 25, 1998

Date
September 25, 1998 · 21:56 local
Place
Orlando, FL
Airport
Orlando Executive Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
FPIA
Damage
Substantial damage
Aircraft
N300EW
NTSB investigation
NTSBATL98LA130
Reported as
Cessna 210L
Reported engine
Continental IO520L
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,500 total800 in this make and model306 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(.19) This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. On September 25, 1998, about 2156 eastern daylight time, a Cessna 210L, N300EW, experienced a landing gear failure while landing at the Orlando Executive Airport, Orlando, Florida. The airplane was operated by flight express as flight 106, under the provision of title 14 CFR part 135, and instrument flight rules. Visual meteorological conditions prevailed and an IFR flight plan was filed. The commercial pilot and sole occupant was not injured, and the airplane sustained substantial damage. The flight originated from Orlando, Florida, the exact time unknown. According to the pilot, an unsafe landing gear indication occurred prior to landing at her distination, saint augustine, Florida. She diverted to craig field in jacksonville, FL, for a visual inspection by the tower personnel. They verified that she had a gear problem. After she talked with her company, it was declined that she return to Orlando, where there was better maintenance and other facitities to deal with the problem. Upon landing gear collapsed, resulting in substantial damage to the airplane. (.4) on September 25, 1998, about 2156 eastern daylight time, a Cessna 210L, N300EW, experienced a landing gear failure while landing at the Orlando Executive Airport, Orlando, Florida. The airplane was operated by flight express as flight 106, under the provisions of title 14 CFR part 135, and instrument flight rules. Visual meteoroglgical conditions prevailed and an IFR flight plan was filed. The commercial pilot and sole occupant was not injured, and the airplane sustained substantial damage. The flight originated from Orlando, Florida, at 1900. According to the pilot, an un-safe landing gear indication occurred prior to landing at her destination, saint augustine, Florida. She diverted to craig field in jacksonville, FL, for a visual inspection by the tower personnel. They were unable to verify that she had a gear problem. The pilot then stuck her head out of the airplanes window to visually inspect the landing gear, allowing her eye glasses to be blown off. After she talked with her company, it was decided that she return to Orlando, where there was better maintenance and other facilities to deal with the problem. Compounding the landing gear problem was the fact that the pilot had to make a night landing without her prescribed eye glasses. Upon landing the main gear collapsed, and the pilot lost control, the airplane did a 180 degree turn on the runway. A post accident inspection of the airplane by company mechanics, revealed a 6-8 inch crack on the right main landing gear actuator, with the actuator housing only half full of hydraulic fluid. They also discovered that the power pack sequencing valve, for the landing gear, was locked up and could not be actuated on the ground. According to a statement by Orlando Executive Airport officials, the airplane landed on runway 13 and all three landing gear partially collapsed, the airplane skidded on the rubber tires and came to rest leaning to the right. Airport officials also stated that, due to the nose high pitch of the airplane, most of the weight of the airplane was supported by the right horizontal stabilizer, resulting in substantial damage to the spar. (-23) aircraft arrived at destination. The gear would not extend. Pilot tried to extend gear manually. Aircraft returned to orl for gear up landing. D uring the flight the pilot stated she opened the window to observe the gear. At this time her glasses fell off. The aircraft landed and turned 180 degrees from direction of flight causing damage to the horizontal stabilizer, and twisting the fuselage, causing substantial damage.

As the FAA filed it

(.19) THIS IS PRELIMINARY INFORMATION, SUBJECT TO CHANGE, AND MAY CONTAIN ERRORS. ANY ERRORS IN THIS REPORT WILL BE CORRECTED WHEN THE FINAL REPORT HAS BEEN COMPLETED. ON SEPTEMBER 25, 1998, ABOUT 2156 EASTERN DAYLIGHT TIME, A CESSNA 210L, N300EW, EXPERIENCED A LANDING GEAR FAILURE WHILE LANDING AT THE ORLANDO EXECUTIVE AIRPORT, ORLANDO, FLORIDA. THE AIRPLANE WAS OPERATED BY FLIGHT EXPRESS AS FLIGHT 106, UNDER THE PROVISION OF TITLE 14 CFR PART 135, AND INSTRUMENT FLIGHT RULES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND AN IFR FLIGHT PLAN WAS FILED. THE COMMERCIAL PILOT AND SOLE OCCUPANT WAS NOT INJURED, AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. THE FLIGHT ORIGINATED FROM ORLANDO, FLORIDA, THE EXACT TIME UNKNOWN. ACCORDING TO THE PILOT, AN UNSAFE LANDING GEAR INDICATION OCCURRED PRIOR TO LANDING AT HER DISTINATION, SAINT AUGUSTINE, FLORIDA. SHE DIVERTED TO CRAIG FIELD IN JACKSONVILLE, FL, FOR A VISUAL INSPECTION BY THE TOWER PERSONNEL. THEY VERIFIED THAT SHE HAD A GEAR PROBLEM. AFTER SHE TALKED WITH HER COMPANY, IT WAS DECLINED THAT SHE RETURN TO ORLANDO, WHERE THERE WAS BETTER MAINTENANCE AND OTHER FACITITIES TO DEAL WITH THE PROBLEM. UPON LANDING GEAR COLLAPSED, RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRPLANE. (.4) ON SEPTEMBER 25, 1998, ABOUT 2156 EASTERN DAYLIGHT TIME, A CESSNA 210L, N300EW, EXPERIENCED A LANDING GEAR FAILURE WHILE LANDING AT THE ORLANDO EXECUTIVE AIRPORT, ORLANDO, FLORIDA. THE AIRPLANE WAS OPERATED BY FLIGHT EXPRESS AS FLIGHT 106, UNDER THE PROVISIONS OF TITLE 14 CFR PART 135, AND INSTRUMENT FLIGHT RULES. VISUAL METEOROGLGICAL CONDITIONS PREVAILED AND AN IFR FLIGHT PLAN WAS FILED. THE COMMERCIAL PILOT AND SOLE OCCUPANT WAS NOT INJURED, AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. THE FLIGHT ORIGINATED FROM ORLANDO, FLORIDA, AT 1900. ACCORDING TO THE PILOT, AN UN-SAFE LANDING GEAR INDICATION OCCURRED PRIOR TO LANDING AT HER DESTINATION, SAINT AUGUSTINE, FLORIDA. SHE DIVERTED TO CRAIG FIELD IN JACKSONVILLE, FL, FOR A VISUAL INSPECTION BY THE TOWER PERSONNEL. THEY WERE UNABLE TO VERIFY THAT SHE HAD A GEAR PROBLEM. THE PILOT THEN STUCK HER HEAD OUT OF THE AIRPLANES WINDOW TO VISUALLY INSPECT THE LANDING GEAR, ALLOWING HER EYE GLASSES TO BE BLOWN OFF. AFTER SHE TALKED WITH HER COMPANY, IT WAS DECIDED THAT SHE RETURN TO ORLANDO, WHERE THERE WAS BETTER MAINTENANCE AND OTHER FACILITIES TO DEAL WITH THE PROBLEM. COMPOUNDING THE LANDING GEAR PROBLEM WAS THE FACT THAT THE PILOT HAD TO MAKE A NIGHT LANDING WITHOUT HER PRESCRIBED EYE GLASSES. UPON LANDING THE MAIN GEAR COLLAPSED, AND THE PILOT LOST CONTROL, THE AIRPLANE DID A 180 DEGREE TURN ON THE RUNWAY. A POST ACCIDENT INSPECTION OF THE AIRPLANE BY COMPANY MECHANICS, REVEALED A 6-8 INCH CRACK ON THE RIGHT MAIN LANDING GEAR ACTUATOR, WITH THE ACTUATOR HOUSING ONLY HALF FULL OF HYDRAULIC FLUID. THEY ALSO DISCOVERED THAT THE POWER PACK SEQUENCING VALVE, FOR THE LANDING GEAR, WAS LOCKED UP AND COULD NOT BE ACTUATED ON THE GROUND. ACCORDING TO A STATEMENT BY ORLANDO EXECUTIVE AIRPORT OFFICIALS, THE AIRPLANE LANDED ON RUNWAY 13 AND ALL THREE LANDING GEAR PARTIALLY COLLAPSED, THE AIRPLANE SKIDDED ON THE RUBBER TIRES AND CAME TO REST LEANING TO THE RIGHT. AIRPORT OFFICIALS ALSO STATED THAT, DUE TO THE NOSE HIGH PITCH OF THE AIRPLANE, MOST OF THE WEIGHT OF THE AIRPLANE WAS SUPPORTED BY THE RIGHT HORIZONTAL STABILIZER, RESULTING IN SUBSTANTIAL DAMAGE TO THE SPAR. (-23) AIRCRAFT ARRIVED AT DESTINATION. THE GEAR WOULD NOT EXTEND. PILOT TRIED TO EXTEND GEAR MANUALLY. AIRCRAFT RETURNED TO ORL FOR GEAR UP LANDING. D URING THE FLIGHT THE PILOT STATED SHE OPENED THE WINDOW TO OBSERVE THE GEAR. AT THIS TIME HER GLASSES FELL OFF. THE AIRCRAFT LANDED AND TURNED 180 DEGREES FROM DIRECTION OF FLIGHT CAUSING DAMAGE TO THE HORIZONTAL STABILIZER, AND TWISTING THE FUSELAGE, CAUSING SUBSTANTIAL DAMAGE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N300EW · 1

Matched to the same aircraft by N-number and date.